The invention discloses a butterfly-shaped aircraft. The aircraft comprises a butterfly-shaped closed aircraft body (10), a power device (30) is fixed in a power channel (20) arranged in the center of the aircraft body (10), an exhaust sealing mechanism (322) is arranged at an exhaust port (321), and a front exhaust port (35), a rear exhaust port (36), a left exhaust port (33) and a right exhaust port (34) are formed in the front side, the rear side, the left side and the right side of the aircraft body (10). The butterfly-shaped aircraft further comprises a control system (40) used for controlling the power device (30), the exhaust sealing mechanism (322), a left exhaust port valve (331), a right exhaust port valve (341), a front exhaust port valve (351) and a rear exhaust port valve (361). According to the technical scheme, the aircraft has the advantages of being good in lifting body structure, high in energy efficiency ratio, simple in structure, low in cost and good in overall rigidity.
一种蝶形飞行器包括呈蝶形封闭的机体(10),在该机体(10)的中心位置设置的动力通道(20)内固定有动力装置(30),在排气口(321)设有排气封闭机构(322),在机体(10)的前后及左右两侧设置有前排气口(35)、后排气口(36)、左排气口(33)和右排气口(34),该蝶形飞行器还包括用于控制所述动力装置(30)、排气封闭机构(322)、左排气口阀门(331)、右排气口阀门(341)、前排气口阀门(351)以及后排气口阀门(361)的控制系统(40)。本发明采用上述的技术方案,可以使这种飞行器具有良好的升力体结构,能效比比较高、结构简单成本低以及整体刚性良好的特点。
Butterfly-shaped aircraft
蝶形飞行器
2021-11-02
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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